# Service difficulty reports: Boeing 767-35H

A list on [Boeing 767-35H](https://openairdocs.org/model/boeing-767-35h.md).

Newest first. General aviation reporting is voluntary.

- [SDR MK1Y20230305001](https://openairdocs.org/sdr/MK1Y20230305001.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Fuselage Structure (General)
  > SEC 43, STA 654 TO 654+22, STR 31L TO 32L: DURING MAINTENANCE INSPECTION, SHOP HAS DISCOVERED A BUCKLE ON FUSELAGE SKIN AT THE NOTED AREA, AND PERFORMED A CUT OUT BY 1.2"X1.5".
- [SDR MK1Y20230305020](https://openairdocs.org/sdr/MK1Y20230305020.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Nacelle/Pylon Structure
  > ENGINE #2 – LH CORE COWL, NAC STA 264.50, UPPER CORNER EDGE: DURING MAINTENANCE INSPECTION, SHOP FOUND A 0.9" LONG CRACK ON AN INCOMING REPAIR AT THE NOTED AREA. IN ADDITION, THE EXISTING REPAIR CONFIGURATION IS MISSING SEAL-FLEX P/N S700S1310-1, FILLER P/N 22
- [SDR MK1Y20230305019](https://openairdocs.org/sdr/MK1Y20230305019.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Nacelle/Pylon Structure
  > ENG #2 FAN COWL OUTER SKIN: 8 (EIGHT) DENTS WERE FOUND WITH CLOSE GAPS IN THE OUTER SKIN OF THE ENG #2 FAN COWL, ON THE OUTBD SIDE BT 4 O'CLOCK TO 5 O'CLOCK.
- [SDR MK1Y20230305018](https://openairdocs.org/sdr/MK1Y20230305018.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Fuselage Main, Plate/Skin
  > REPAIR – EXTERNAL FUSELAGE SKIN, STA 1809 TO 1824, 4.0" ABOVE STR 22R: DURING MAINTENANCE INSPECTION AT IAI, SHOP FOUND AN UNDOCUMENTED DOUBLER REPAIR AT THE NOTED AREA. SIZE: 14.5"X15.5".
- [SDR MK1Y20230305017](https://openairdocs.org/sdr/MK1Y20230305017.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Doors
  > : R/H MAIN LANDING GEAR TRUNNION DOOR AT OUTER SKIN, FWD EDGE LOWER CORNER: DURING MAINTENANCE INSPECTION, SHOP FOUND UNDOCUMENTED DOUBLER REPAIR AT THE NOTED AREA.DIMENSION OF DOUBLER REPAIR: 6.0"X7.5".
- [SDR MK1Y20230305016](https://openairdocs.org/sdr/MK1Y20230305016.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Nacelle/Pylon Structure
  > ENGINE #2 CF6-80C2B6F, EXHAUST, NAC STA 332.34 AND NAC STA 360.73: SHOP FOUND A DENT WITH SHARP CREASE ON THE EXTERNAL EXHAUST SKIN LOCATED ON ENGINE 2 NAC STA 332.34, BT 6 TO 5 O’CLOCK. SIZE: L=0.50”, Y=0.020, A=0.47 A/Y=23. IN ADDITION, SHOP FOUND ANOT
- [SDR MK1Y20230305015](https://openairdocs.org/sdr/MK1Y20230305015.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Nacelle/Pylon Structure
  > ENGINE #2 CF6-80C2B6F STRUT, AFT FAIRING PANEL ASSY, BETWEEN NAC STA 304.54 AND NAC STA 308.00: SHOP FOUND AN EXISTING REPAIR ON THE OUTBD SIDE OF STRUT #2 IN THE OUTER SKIN PANEL LOCATED BELOW ACCESS DOOR BT NAC STA 304.54 TO 308.00. SIZE OF THE REPAIR: 3.5"X
- [SDR MK1Y20230305013](https://openairdocs.org/sdr/MK1Y20230305013.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Nacelle/Pylon Structure
  > ENGINE # 2 OUTBD CORE COWL SKIN: DURING MAINTENANCE INSPECTION AT IAI FOUND UNDOCUMENTED DOUBLER REPAIR ENG # 2 OUTBD CORE COWL AROUND FWD LATCH CUTOUT BT NAS STA 264.37 TO 270.57 AT 6 O’CLOCK.
- [SDR MK1Y20230305012](https://openairdocs.org/sdr/MK1Y20230305012.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Nacelle/Pylon Structure
  > ENGINE #2 INBD CORE COWL SKIN: DURING MAINTENANCE INSPECTION AT IAI FOUND EXISTING HAT FRAME REPAIR NOT ACCORDING TO SRM ON INBD CORE COWL ENG #2 NAC STA 303.75 BT 11 TO 12 O’CLOCK.EXTERNAL DOUBLER SIZE: 1.7”X7.1”. ENGEL PATCH SIZE: 6”X4” APP. P/N: 224-2301-51
- [SDR MK1Y20230305011](https://openairdocs.org/sdr/MK1Y20230305011.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Nacelle/Pylon Structure
  > ENGINE #2, BT NAC STA 268.7 TO 303.7 AND BT 9 TO 10 O'CLOCK: DURING MAINTENANCE INSPECTION SEVERAL SCRATCHES DAMAGE WERE FOUND ON CORE COWL SKIN. FASTENERS REMOVED, AND INSTALLED AFTER THE AREA WAS BLENDED PER SRM 51-40-02. SMOOTHING WAS PERFORMED IN THE AREA
- [SDR MK1Y20230305010](https://openairdocs.org/sdr/MK1Y20230305010.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Nacelle/Pylon Structure
  > ENGINE #1 OUTBD CORE COWL SKIN: DURING MAINTENANCE INSPECTION AT IAI FOUND TWO EXISTING UNDOCUMENTED DOUBLER REPAIRS ON OUTBD CORE COWL. M0149 – LOCATED NAC STA 268 TO 283 AT 6 O'CLOCK SIZE 15"X4.8". M0151 – LOCATED NAC STA 303.75 BT 11 TO 12 O'CLOCK SIZE 1.6"
- [SDR MK1Y20230305009](https://openairdocs.org/sdr/MK1Y20230305009.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Nacelle/Pylon Structure
  > STRUT FAIRING SKIN, INBD SIDE: EXISTING UNDOCUMENTED 2.8"X1.4" DOUBLER REPAIR ON THE INBD SIDE OF STRUT FAIRING SKIN BELOW DOOR PANEL BT STA 304.54 – 307.34.
- [SDR MK1Y20230305008](https://openairdocs.org/sdr/MK1Y20230305008.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Fuselage Structure (General)
  > DURING MAINTENANCE INSPECTION AT IAI, A DENT WAS FOUND ON THE LOWER SKIN PANEL OF LAP SPLICE AT STR 36L, STA 1433 (BELOW BULK CARGO DOOR). DENT DIMENSIONS: L=2.24", A=1.95, Y=0.050, A/Y=39.
- [SDR MK1Y20230305007](https://openairdocs.org/sdr/MK1Y20230305007.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Doors
  > SEC 48, STA 1854 TO 1863: FOUND EXISTING DOUBLER REPAIR ON RH DOOR EXTERNAL SKIN AROUND LATCH CUTOUT LOWER LONGERON.
- [SDR MK1Y20230305006](https://openairdocs.org/sdr/MK1Y20230305006.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Fuselage Structure (General)
  > DURING MAINTENANCE INSPECTION, AIRCRAFT MAINTENANCE CORRODED AREA WAS FOUND AT DRAIN MUST BETWEEN STA 1395 AND STA 1417 AND STR 35R AND STR 36R. A UT INSPECTION WAS ACCOMPLISHED ON BLENDED AREA TO DETERMINE THE REMAINING MATERIAL THICKNESS AS CONTAINED
- [SDR MK1Y20230305005](https://openairdocs.org/sdr/MK1Y20230305005.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Fuselage Structure (General)
  > FUSELAGE SKIN, STA 325 BT STR21L-22L: TWO EXISTING BLENDOUTS FOUND ON EXTERNAL FUSELAGE SKIN. NOMINAL THICKNESS: 0.130". (-0.002" THICKNESS BLENDED). ONLY ONE BLENDOUT IS DOCUMENTED.
- [SDR MK1Y20230305004](https://openairdocs.org/sdr/MK1Y20230305004.md): None · none · Mar 5, 2023 · N206CM · Boeing 76735H · Fuselage Structure (General)
  > SECTION 41 – FUSELAGE SKIN AT STA 159.5 AND ABOVE STR30R: DURING MAINTENANCE INSPECTION, EXISTING BLEND OUT AND LIGHTING STRKE WERE FOUND. SKIN P/N 141T3211, IS MADE FROM 0.08” CLAD 2024-T3 (CHEM-MILLED 0.045”0. THE BLEND OUT IS BEYOND LIMITS PER SRM 53-00-01,
- [SDR I5EA2022061700002](https://openairdocs.org/sdr/I5EA2022061700002.md): Slide Raft · deployed · Jun 16, 2022 · N827RC · Boeing 76735H · Emergency Equipment
  > INADVERTENT ESCAPE SLIDE/RAFT DEPLOYMENT DURING MAINTENANCE ACTIVITIES, REPLACED L1 DOOR ESCAPE SLIDE/RAFT IAW B767 AMM 25-66-01. MDL 32515 ITEM 2
- [SDR CA150318012](https://openairdocs.org/sdr/CA150318012.md): Ballast · burned · Mar 17, 2015 · Boeing 76735H · Passenger Compartment Lighting
  > (CAN) AS REPORTED BY CABIN CREW, ODOR OF BURNING WIRES VERY STRONG AROUND ROW 20 AND 21. FOUND BALLAST AT 21AC WITH BLOWN FUSE AND BURNED ELECTRICAL ODOR. REPLACED BALLAST AND CHECKED SERVICE.
- [SDR CA141128001](https://openairdocs.org/sdr/CA141128001.md): Module · failed · Nov 27, 2014 · Boeing 76735H · Trailing Edge Flap Control System
  > (CAN) AIR RETURN DUE TO FLAP DISAGREE, PAN PAN DECLARED, OVERWEIGHT LANDING. RESOLUTION CENTER FLAP/STABILIZER POSITION MODULE M839 REPLACED AND FUNCTION CHECKED OK, REF AMM 27-58-01, PB 401. SEE L5171130 FOR RECTIFICATION OF THE SYSTEM 2 NOSE GEAR AIR/GROUN
- [SDR CA140826024](https://openairdocs.org/sdr/CA140826024.md): Oil System · leaking · Aug 22, 2014 · Boeing 76735H · Turbine Engine Oil System
  > (CAN) DURING THE ATLANTIC CROSSING, OIL BEGAN TO DIMINISH ON THE RIGHT ENGINE. QUANTITY FELL TO ZERO AND THE DECISION WAS MADE TO HAVE THE FLIGHT DIVERTED. A PAN WAS DECLARED. THE FLIGHT LANDED WITHOUT FURTHER EVENT AND THE ENGINE WAS SHUT DOWN IMMEDIATELY AFT
- [SDR CA121221008](https://openairdocs.org/sdr/CA121221008.md): Skin · corroded · Dec 15, 2012 · Boeing 76735H · Fuselage Main, Plate/Skin
  > (CAN) CORROSION FOUND ON FUSELAGE SKIN AT THE FORWARD LAVATORY BLOWER VENT OUTLET. EXFOLIATION CORROSION BETWEEN. LT FS SKIN BS 1540-1562, BETWEEN STR 24L-25L WAS TEMPORARY REPAIRED PENDING DTA.
- [SDR CA120514002](https://openairdocs.org/sdr/CA120514002.md): Seal · departed · May 12, 2012 · Boeing 76735H · Ailerons
  > (CAN) ON APPROACH, FLAP, AILERON SEAL CAME OFF IN FLIGHT. MOC ADVISED. LANDED WITHOUT INCIDENT. ON RT WING, T/E BETWEEN INBD AND NEXT FLAP, RUBBER SEAL FLAPPING IN THE WIND IN FLIGHT, FELL OFF ON APPROACH. FOUND ON RT INBD AILERON UPPER SEAL MISSING, DEPAR
- [SDR CA110105007](https://openairdocs.org/sdr/CA110105007.md): Buss · failed · Jan 4, 2011 · Boeing 76735H · Electrical Power System Wiring
  > AS A RESULT OF A MALFUNCTION OF THE ELECTRICAL BUSES, THE FLIGHT ELECTED TO RETURN WITH SUBSEQUENT OVERWEIGHT LANDING. REPEAT SNAG, L/R UTILITY BUSS OFF LIGHTS, EICAS MESSAGE, L/R RECIRC FANS OFF LIGHTS WITH LOSS OF GALLEY POWER AND PAX READING LIGHTS U/S. I
- [SDR CA110103006](https://openairdocs.org/sdr/CA110103006.md): Wire · broken · Jan 2, 2011 · Boeing 76735H · Instrument System Wiring
  > FLIGHT RETURNED TO DUE RED EICAS FLAP/SLAT ALERT T/O CONFIG, LANDING NORMAL. FINDINGS LISTED SEQ 2 DIODE BLOCK R608 PIN LOCK BROKEN AND LOOSE WIRE. DIODE BLK R608 REPLACED. ALSO L FSPM REPLACED AND TESTED IAW AMM 27-58-01-904-001. WEU PCC REPLACED AND TESTE
- [SDR CA101019007](https://openairdocs.org/sdr/CA101019007.md): Valve · failed · Oct 18, 2010 · Boeing 76735H · Brake Anti-Skid Section
  > DURING THE APPROACH TO LAND, THE CREW ADVISED THEY HAD AN ANTI-SKID FAILURE AND WERE REQUESTING A LONGER RUNWAY FOR THE LANDING. THE LANDED WITHOUT USING THE ANTISKID AND WITHOUT INCIDENT. INBD ANTI-SKID BITE VALVE 7 FAULT ANTI-SKID NORMAL AND ALT TEST NO FA
- [SDR CA080229007](https://openairdocs.org/sdr/CA080229007.md): Lever · misinstalled · Feb 20, 2008 · Boeing 76735H · Escape Slide
  > (CAN) OVER-WING SLIDE COMPARTMENT DOOR OPENING ACTUATING MECHASIM - LEVER DESCRIPTION: A LEVER THAT JOINS THE FIRING PIN CLEVIS OF THE OFF-WING ESCAPE SLIDE COMPARTMENT DOOR OPENING ACTUATOR TO THE ACTUATING ROD IS BEING INSTALLED UPSIDE-DOWN. THIS APPEARS TO
- [SDR CA040216001](https://openairdocs.org/sdr/CA040216001.md): Odor · detected · Feb 16, 2004 · Boeing 76735H · Air Distribution System
  > (CAN) THE FLIGHT EXPERIENCED AN ACRID ODOR IN THE COCKPIT. AC DECLARED AN EMERGENCY LANDING AND CARRIED OUT THE QRH. AC SENT TO HANGAR FOR INVESTIGATION.
- [SDR CA040120005](https://openairdocs.org/sdr/CA040120005.md): Engine · flamed out · Jan 20, 2004 · Boeing 76735H · Engine (Turbine/Turboprop)
  > (CAN) ON TAXI OUT LT ENGINE FLAMED OUT, WITH OIL ODOR IN THE CABIN. RETURNED TO GATE, AIRCRAFT CHANGED, ENGINE REPLACED IAW 71-00-02 CONF.
- [SDR CA020826003](https://openairdocs.org/sdr/CA020826003.md): Cooling Fan · failed · Aug 15, 2002 · Boeing 76735H · Air Distribution Fan
  > (CAN) INTERMITTENT LOUD SQUEEL IN FRONT CABIN AND GALLEY WAS FOLLOWED BY MOMENTARY SMOKE IN FLIGHT DECK AND FWD EQUIPMENT BAY FAN STATUS MESSAGE WITH ASSOCIATED CB POPPING.FORWARD EQUIPMENT COOLING FAN REPLACED AS PER AMM.
- [SDR EVAS91015](https://openairdocs.org/sdr/EVAS91015.md): Tiller · failed · Aug 6, 2002 · N16605 · Boeing 76735H · Landing Gear Steering System
  > TILLER STEERING RIGHT ONLY DURING TAXI, REPLACED NLG STEERING METERING VALVE & RIGGING & OPR CHECKED NORMAL.
- [SDR CA010105002](https://openairdocs.org/sdr/CA010105002.md): Spur Gear · damaged · Dec 11, 2000 · Boeing 76735H · Pressure Regulator/Outflow Valve
  > (CAN) REMOVED ACTUATOR FROM A/C DUE REPEAT PIREP. SHOP INSPECTION FOUND SPUR GEAR SPLINE HAD A SEGMENT MISSING. THIS MISSING SEGMENT HAD BEEN REPLACED BY A ROLL PIN LAID IN THE OPEN AREA OF THE SPLINE. NO APPROVED REPAIR ALLOWS THE USE OF ROLL PINS IN REPAIRS
- [SDR CA001214005](https://openairdocs.org/sdr/CA001214005.md): Shaft · missing · Dec 11, 2000 · Boeing 76735H · Pressure Regulator/Outflow Valve
  > (CAN) REMOVED ACTUATOR FROM A/C DUE REPEAT PREP. SHOP INSPECTION FOUND SPUR GEAR SPLINE HAD A SEGMENT MISSING. THIS MISSING SEGMENT HAD BEEN REPLACED BY A ROLL PIN LAID IN THE OPEN AREA F THE SPLINE. NO APPROVED REPAIR ALLOWS THE USE OF ROLL PINS IN REPAIRS T
- [SDR 95ZZZX4543](https://openairdocs.org/sdr/95ZZZX4543.md): Support Rod · broken · Jun 11, 1995 · N800CZ · Boeing 76735H · Potable Water System
  > THE CREW REPORTED THERE WAS WATER LEAKAGE. AFT-FLIGHT CHECK FOUND FOUR RODS FOR LEFT WATER TANK SUPPORT BROKEN AND THE SUPPORT CRACKED. THE AIR TUBE BESIDE THE WATER TANK WAS PRESSED OUT OF SHAPE. RECOMMEND TO REPLACE THE FOUR RODS AND REPAIR THE WATER TANK

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '76735H'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-35h/reports

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